JPS6089605A - Combustion method for fuel oil - Google Patents

Combustion method for fuel oil

Info

Publication number
JPS6089605A
JPS6089605A JP19612983A JP19612983A JPS6089605A JP S6089605 A JPS6089605 A JP S6089605A JP 19612983 A JP19612983 A JP 19612983A JP 19612983 A JP19612983 A JP 19612983A JP S6089605 A JPS6089605 A JP S6089605A
Authority
JP
Japan
Prior art keywords
combustion
oil
fuel oil
fuel
self
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP19612983A
Other languages
Japanese (ja)
Inventor
Kazuo Kino
城野 一男
Hidekatsu Ikeda
池田 秀克
Shinya Naka
中 信也
Yuunosuke Tsukioka
月岡 雄之弼
Hidenobu Katada
堅田 秀信
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Gas Chemical Co Inc
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Gas Chemical Co Inc
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Gas Chemical Co Inc, Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Gas Chemical Co Inc
Priority to JP19612983A priority Critical patent/JPS6089605A/en
Publication of JPS6089605A publication Critical patent/JPS6089605A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)

Abstract

PURPOSE:To contrive to ensure a combustion system having a high turndown ratio, by a method wherein a fuel oil and a self-burning gas serving as a spray medium are fed to a fuel oil feed cylinder incorporating a mixer, and the self- burning gas is used as assistant combustion for the fuel oil. CONSTITUTION:A mixer 2 consists of a fuel flow pore 5, a self-burning gas flow pore 6, and a mixing chamber 7, and a fuel oil A and a self-burning gas B are fed in the mixing chamber 7 through pores 5 and 6 by means of feed pipes 3 and 4, respectively, to mix them together. The oil-gas mixture fuel is discharged through injection nozzles 8 formed in the forward end of the body of a feed cylinder 1, and in this case, the mixture fuel is injected and sprayed by means of a movement amount of the fuel oil itself for combustion. This causes increasing of an assistant combustion effect on an oil drop 11 by means of the combustion heat of a self-burning gas layer 13 on the outer surface of the oil drop 11 is high, and as a result, a rate is seldom determined by means of an oil drop of size and a relative speed 14 between the oil drop and the atmosphere.

Description

【発明の詳細な説明】 本発明は燃料油の燃焼方式に関する。[Detailed description of the invention] The present invention relates to a fuel oil combustion method.

管式加熱炉、ボイラ及びその他の燃焼炉に設置される燃
焼器(バーナー)は、当該炉の性能を支配する重要な構
成機器であって、このために燃焼器に要求される主要な
機能としては、(7)プロセスの要求に応じた負荷範囲
内において安定燃焼が達成できること、(f)火炎形状
が良好なこと、(つ)過剰空気が少ないこと、に)燃料
油燃焼の場合特に燃料油噴射孔(バーナーチップ)での
燃料油の閉塞がないこと、(3)NOx (窒素酸化物
)発生が少ないこと、等が挙げられる。
The combustor (burner) installed in tube heating furnaces, boilers, and other combustion furnaces is an important component that controls the performance of the furnace, and for this purpose, the main functions required of the combustor are: (7) Stable combustion can be achieved within the load range according to process requirements, (f) Good flame shape, (1) Less excess air, and (7) In the case of fuel oil combustion, especially fuel oil (3) There is no clogging of fuel oil in the injection hole (burner tip), and (3) there is little generation of NOx (nitrogen oxides).

ここで燃料油燃焼器については、従来の代表的燃焼方式
として次の3つの方法がある。
Here, regarding fuel oil combustors, there are the following three methods as typical conventional combustion methods.

(1ン 蒸気噴霧方式 本方式は油燃焼の主流を占めるものであシ油を霧化させ
るために、蒸気を用いる。蒸気としては一般に過熱蒸気
が用いられ、蒸気噴霧量は燃料油に対し約10〜50重
量%を必要とし、蒸気圧力は油圧よシ約1〜5 )c!
$ / cm”高く供給される。
(1) Steam spray method This method is the mainstream of oil combustion and uses steam to atomize the oil. Superheated steam is generally used as the steam, and the amount of steam sprayed is approximately Requires 10-50% by weight, steam pressure is about 1-5) c!
Supplied at a high price of $/cm”.

(11)高圧空気噴霧方式 上記(+〕の蒸気に代え空気にて油を霧化させる。空気
噴霧量は理論燃焼空気量の2〜10チ必要でアシ、空気
圧力は(1)と同様油圧より約1〜l//口2高く供給
される。
(11) High-pressure air atomization method Atomizes the oil with air instead of steam (+) above.The amount of air sprayed is 2 to 10 inches of the theoretical combustion air amount, and the air pressure is the same as in (1), which is oil pressure. It is fed approximately 1 to 1/2 mouths higher than the standard.

亜 油圧噴霧方式 本方式は噴霧媒体を用いず加圧加温した油を小孔を通過
させることによって霧化する。
Sub-hydraulic spraying method This method does not use a spraying medium and atomizes pressurized and heated oil by passing it through small holes.

この場合の油圧は5〜5 ’ Okg/ m2G程度に
上げる必要がある。
In this case, the oil pressure needs to be raised to about 5 to 5'Okg/m2G.

しかし、以上述べた従来の代表的燃料油燃焼方式に共通
する欠点は、安定燃焼範囲即ち〔最小燃焼量/最大燃焼
量(ターンダウンレイジオTurn Dovrn Ra
tio) )が約173〜1/4程度と小さいことでお
る。
However, a common drawback of the conventional typical fuel oil combustion methods described above is the stable combustion range, that is, [minimum combustion amount/maximum combustion amount (Turn Dovrn Ra
tio) ) is as small as about 173 to 1/4.

本発明者は従来法よシもターンダウンレシオの大きい燃
焼方式の確立を目的とし研究努力の結果、従来型の蒸気
或いは高圧、低圧空気に代えて自燃性ガスを用いること
によシ燃料油の安定燃焼範囲を0〜100%とでき、上
記目的を達成し得ることを見出し本発明に到った。
As a result of research efforts aimed at establishing a combustion method with a higher turndown ratio than conventional methods, the inventors of the present invention have discovered that they can reduce fuel oil by using combustible gas in place of conventional steam or high-pressure or low-pressure air. It was discovered that the stable combustion range can be set to 0 to 100% and the above object can be achieved, leading to the present invention.

すなわち本発明の要旨とするところは、混合器を内蔵す
る燃料油供給筒に、燃料油と噴霧媒体としての自燃性ガ
スを供給し、該自燃性ガスを上記燃料油の助燃に用いる
ことを特徴とする燃料油燃焼方法の方法を提供するとこ
ろにある。
That is, the gist of the present invention is to supply fuel oil and a self-combustible gas as an atomizing medium to a fuel oil supply tube incorporating a mixer, and to use the self-combustible gas for auxiliary combustion of the fuel oil. The present invention provides a method for burning fuel oil.

本発明の方法の特徴を従来法と比較すると以下の如くで
ある。
The characteristics of the method of the present invention are as follows when compared with the conventional method.

fl) 燃焼機構の考え方 従来方式;油滴を微粒化し燃焼性確保 本発明;自燃性ガスによる助燃効果(アシストバーニン
グ)による燃焼性確 保(操作条件の設定)。
fl) Combustion mechanism concept Conventional method; Oil droplets are atomized to ensure combustibility. Present invention; combustibility is ensured by the auxiliary combustion effect (assist burning) of self-combustible gas (setting of operating conditions).

(2) 噴霧媒体の供給圧力(最大燃焼時)従来型;油
圧グラス1 kIt/ cm”以上本発明;油圧プラス
5 kg / cm”以下でよい(3)噴霧媒体の種類 従来型;蒸気、高圧及び低圧空気 本発明;自燃性ガス (4)燃焼速度 従来型:急速燃焼 本発明1緩慢燃焼 (5) NO!低減効果 従来型;無し 本命F!A:■ (4)項の緩慢燃焼 ■ 自燃性ガス(還元性ガス)に よるフレーム中でのNOX還元反 応 上記■、■による低減効果有 (従来型より20%以上の低減有 り) 本発明における自燃性ガスとしては、発熱量(L、H,
V、すなわちLow HeatingValue :燃
料の真発熱量であって、燃料を燃焼した際の単位熱量@
シの発熱量をいう。Kcal/ Mm”又はKcal/
 k?で表す)を持つガスであればいずれでもよく、例
えば天然ガス、H2、OH,を含む石油精製オフガス等
炭化水素系ガス等が挙げられ、又、NOx低減効果を発
揮できる対象としては、上記の炭化水素系ガスであれば
いずれでもよい。
(2) Supply pressure of spray medium (maximum combustion) Conventional type: Hydraulic glass 1 kIt/cm" or more Invention: Hydraulic pressure plus 5 kg/cm" or less (3) Type of spray medium Conventional type: Steam, high pressure and low pressure air Invention; flammable gas (4) Burning speed Conventional type: Rapid combustion Invention 1 Slow combustion (5) NO! Reduction effect conventional type; No favorite F! A: ■ Slow combustion in item (4) ■ NOx reduction reaction in the flame due to flammable gas (reducing gas) Reduction effect due to the above ■ and ■ (20% or more reduction compared to conventional type) Self-combustion in the present invention The calorific value (L, H,
V, or Low Heating Value: The net calorific value of the fuel, which is the unit calorific value when burning the fuel @
It refers to the calorific value of shi. Kcal/ Mm” or Kcal/
k? For example, natural gas, hydrocarbon gas such as oil refining off-gas containing H2, OH, etc. can be used as long as it has a NOx reduction effect. Any hydrocarbon gas may be used.

以下本発明を図によシ具体的に説明する。The present invention will be specifically explained below with reference to the drawings.

第1図は従来からある燃料油供給筒(オイルガン)の−
例を示すものであって、本発明で用いる燃料油供給筒は
この従来型の構造のものでよい。
Figure 1 shows a conventional fuel oil supply tube (oil gun).
This is just an example, and the fuel oil supply tube used in the present invention may have this conventional structure.

燃料油供給筒1は、混合器(アトマイザ−)2、燃料給
供管3、及び自燃性ガス供給管4よシ成っている。(従
来方式では4は噴霧媒体供給管として用いる。ン混合器
2は燃料油流通細孔5、自燃性ガス流通則孔6及び混合
室7よシ成っていて、燃料油A及び自燃性ガスBはそれ
ぞれの供給管3及び4より各細孔5及び6を通シ混合室
7内に供給され混合される。この油−ガス混合燃料は供
給筒1の本件先端に設けられた噴出孔8から放出される
が、この時燃料油自体の運動量によって噴出霧化され、
燃焼する。
The fuel oil supply pipe 1 is made up of a mixer (atomizer) 2, a fuel supply pipe 3, and a self-combustible gas supply pipe 4. (In the conventional system, 4 is used as an atomizing medium supply pipe. is supplied from the respective supply pipes 3 and 4 through the small holes 5 and 6 into the mixing chamber 7 and mixed therein. However, at this time, the momentum of the fuel oil itself causes it to be sprayed out and atomized.
Burn.

霧化された燃料油部の燃焼機構を、従来方式の一例であ
る蒸気噴霧方式と比較した第2図を用いて説明する。
The combustion mechanism of the atomized fuel oil section will be explained using FIG. 2, which compares it with a steam spray method, which is an example of a conventional method.

第2図(a)は従来方式による油滴の燃焼を、又、同(
1))は本発明の方式によるものを示していて、図中1
1は単一油滴、12は燃焼面、13は自燃性ガス層、そ
して14は相対流速を示している。
Figure 2 (a) shows the combustion of oil droplets by the conventional method, and the same (
1)) shows the method of the present invention, and 1 in the figure
1 is a single oil droplet, 12 is a combustion surface, 13 is a self-combustible gas layer, and 14 is a relative flow velocity.

第2図(a)の従来方式の場合、油滴11は、燃焼面1
2全通しての外側の高温空気からの伝熱によシ蒸発気化
して燃焼する。
In the conventional method shown in FIG. 2(a), the oil droplet 11 is
2. It evaporates and burns due to heat transfer from the high temperature air on the outside.

これに対し第2図(′b)に示す本発明の方法において
は、単一油滴11の外側には自燃性ガス層13が形成さ
れる。したがって燃焼面12を通しての外側の高温空気
からの伝熱によって自燃性ガス層13の燃焼が起こると
同時に油滴11は蒸発気化して燃焼する。
In contrast, in the method of the present invention shown in FIG. 2('b), a self-combustible gas layer 13 is formed outside the single oil droplet 11. Therefore, the oil droplet 11 evaporates and burns at the same time as the combustion of the self-combustible gas layer 13 occurs due to heat transfer from the outside high-temperature air through the combustion surface 12.

ここで重要なこととして、蒸気噴霧方式の場合、燃焼性
確保の為、■噴霧蒸気圧力を燃料油の油圧以上に高め油
滴を微粒化すること及び■乱流拡散のため燃焼室内にお
ける空気の流速との相対速度(燃焼炉中において、燃料
の燃焼により発生する燃焼ガスの流れと、液滴の落下又
は上昇速度の相対比較をいう)14を高めることの2点
が必須条件として挙げられる。燃料と空気の各々の流速
が減少すれば混合悪化となり燃焼不良を生じる。燃料流
速が小、空気流速が犬の場合は吹き消え、逆に空気流速
が小さすぎると不完全燃焼を引き起す。従って燃料と空
気の流速の最適な差(すなわち最適な相対速度)及び両
者のある絶対流速確保が燃焼の安定性に寄与する。
It is important to note here that in the case of the steam atomization method, in order to ensure combustibility, the pressure of the spray steam must be raised above the hydraulic pressure of the fuel oil to atomize the oil droplets, and ■ The air in the combustion chamber must be Two essential conditions are to increase the relative velocity (relative comparison between the flow of combustion gas generated by combustion of fuel in a combustion furnace and the falling or rising velocity of droplets) 14. If the respective flow velocities of fuel and air decrease, the mixing will deteriorate, resulting in poor combustion. If the fuel flow rate is low and the air flow rate is low, it will blow out, and if the air flow rate is too low, incomplete combustion will occur. Therefore, an optimal difference between the flow velocities of fuel and air (that is, an optimal relative velocity) and ensuring a certain absolute flow velocity of both contribute to the stability of combustion.

これに対し本発明の方法では、油滴11外面の自燃性ガ
ス層15の燃焼熱による油滴11に対する助燃効果が大
きいために、上記蒸気噴霧方式に比べて、油滴径及び大
気との相対速度14によシ律速されることが少ない。(
低燃焼域では油噴霧速度が低下するため、必然的に相対
速度が低下する。) 以上の作用よp従来法と比較した本発明の効果は次の如
くである。
On the other hand, in the method of the present invention, since the combustion heat of the combustible gas layer 15 on the outer surface of the oil droplet 11 has a large auxiliary combustion effect on the oil droplet 11, the diameter of the oil droplet and the relative relationship with the atmosphere are greater than in the steam spray method. The speed is rarely limited by the speed 14. (
Since the oil spray speed decreases in the low combustion range, the relative velocity inevitably decreases. ) The effects of the present invention compared with the conventional method are as follows.

1)油滴微粒化は従来方式程の微粒にする必要がなく、
このため自燃性ガス圧力を油圧以下にしても燃焼できる
。好ましいガス圧としては燃焼油圧プラス5 kg /
 on2以下である。
1) Oil droplet atomization does not need to be as fine as the conventional method,
Therefore, combustion is possible even if the combustible gas pressure is lower than the hydraulic pressure. The preferred gas pressure is combustion oil pressure plus 5 kg/
on2 or less.

i1ン 大気との相対速度は従来法以下でよいため、燃
料油の安定燃焼範囲はガスが存在する限シ、0〜100
%を確保できる。
Since the relative velocity with the atmosphere can be lower than the conventional method, the stable combustion range of fuel oil is 0 to 100 as long as gas is present.
% can be secured.

111)燃料油燃焼は自燃性ガスの燃焼を介した燃焼の
だめ、緩慢燃焼となり、かつ、自燃性ガスの還元作用に
よシ自燃性ガス及び油M燃焼過程において酸素の存在下
900〜1500℃において、NOXの還元反応が生じ
る。以上よJ NOXの低減効果がある。
111) Fuel oil combustion is a slow combustion due to the combustion of flammable gas, and due to the reduction action of flammable gas. , a reduction reaction of NOX occurs. As described above, there is an effect of reducing J NOx.

以上の本発明の方法の効果について実証データを実施例
1及び比較例1の結果を挙げて具体的に示す。
Demonstrative data regarding the effects of the above method of the present invention will be specifically shown by citing the results of Example 1 and Comparative Example 1.

1、実施例1 第1図に示した装置を用い、下記の燃焼油及び自燃性ガ
スを用いて燃焼を行った。各条件及び得られた火炎長さ
等を第1表にまとめて示す。
1. Example 1 Using the apparatus shown in FIG. 1, combustion was carried out using the following combustion oil and self-combustible gas. Table 1 summarizes each condition and the obtained flame length.

第 1 表 燃料油性状:す7?比重 15/4℃ 0.76粘度(
cp) 0.66 組成(wt%) 0:86.H=14 LHV (Kcal/に? ) 10.500自燃性ガ
ス;天然ガス LHV=9450Kcal、/輻”ここ
で空気過剰率については、第1図に示す装置を囲む風箱
に設置された空気調節用格子を開閉して調節した。
Table 1 Fuel oil properties: Su7? Specific gravity 15/4℃ 0.76 viscosity (
cp) 0.66 Composition (wt%) 0:86. H=14 LHV (Kcal/in?) 10.500 Self-combustible gas; natural gas LHV=9450 Kcal,/radius Here, regarding the excess air ratio, the air conditioning installed in the wind box surrounding the device shown in Figure 1. Adjustments were made by opening and closing the grid.

また火炎長は、炉体の大きさに制限があるため、異常に
長炎又は短炎となると不均一加熱と力って生産炉等では
性能確保が困難となる。一般的な火炎長としては1〜4
tytである。
Further, since the flame length is limited by the size of the furnace body, an abnormally long or short flame will cause uneven heating, making it difficult to maintain performance in a production furnace or the like. The general flame length is 1 to 4.
It is tyt.

従来法の場合通常燃料油の安定燃焼範囲は、最小燃焼量
/最大燃焼量チとして50〜100チである。これに対
し本発明の方法はテスト番号79での燃焼量6 & 2
 ky/Hを100%とする時にテスト番号80では0
%、テスト番号104では約11チであって、安定燃焼
範囲は0〜100%と、従来法に比して明らかに巾が広
がっていることが第1表よりわかる。
In the case of the conventional method, the stable combustion range of normal fuel oil is 50 to 100 degrees as the minimum combustion amount/maximum combustion amount. On the other hand, the method of the present invention has a combustion amount of 6 & 2 in test number 79.
When ky/H is 100%, test number 80 is 0
%, test number 104 was about 11 inches, and it can be seen from Table 1 that the stable combustion range was 0 to 100%, clearly wider than the conventional method.

1比較実験例1 第1図に示す装置を用い本発明の方法の自燃性ガス噴霧
の場合と、従来法の蒸気噴霧方法による場合を比較した
。各条件及び得られた結果は第2表にまとめて示すとお
シであった。
1 Comparative Experimental Example 1 Using the apparatus shown in FIG. 1, a comparison was made between the method of the present invention using self-combustible gas spraying and the conventional steam spraying method. The conditions and the results obtained are summarized in Table 2.

第 2 表 燃料油性状;C重油 AP工Gr注> (6[]’F) 15.8LHV =
 10.800 Kcal/に9自m 性カス; 天然
i スLHV =9450 KcaVNm’注 AP工
 Gr : American Petroleum工
n5titute Gravity 第2表から本発明の方法の燃料油圧力は従来の蒸気噴霧
法の13kg/−に比して21〜2.6に9 / cr
n2Gと低くてすみ、自燃性ガスの圧力も蒸気を噴霧す
る圧力よりはるかに低圧でよい上に、NOX レベ# 
(ppm )も6%o、 換算で145.159 pp
mと蒸気噴霧法の187.214 ppmよシも少ない
。すなわちNOXの低減効果が明らかに認められる。
Table 2 Fuel oil properties; C heavy oil AP engineering Gr Note>(6[]'F) 15.8LHV =
10.800 Kcal/9 self-mass; Natural Is LHV = 9450 KcaVNm' Note AP engineering Gr: American Petroleum engineering n5 titute Gravity From Table 2, the fuel oil pressure of the method of the present invention is 13 kg compared to the conventional steam spray method. 9/cr to 21-2.6 compared to /-
n2G, the pressure of the combustible gas can be much lower than the pressure for atomizing steam, and the NOX level #
(ppm) is also 6%o, converted to 145.159 pp
m and 187.214 ppm for the steam atomization method. That is, the effect of reducing NOX is clearly recognized.

以上I、■に示したデータより本発明の方法による効果
すなわち燃料油の安定燃焼範囲が0〜100%と巾広く
、かつ、NOXを低減することは明らかであシ、本発明
の方法は各種バーナー単体、各種バーナーを設置する装
置(例えばボイラ、加熱炉、インジオレータ、焼却炉等
)に応用しうるのみならず、上記のような既設装置中の
従来方式バーナーにおいても混合器を交替するのみで容
易に改造しうる実用性の高い方法である。
From the data shown in I and (2) above, it is clear that the effect of the method of the present invention, that is, the stable combustion range of fuel oil is wide from 0 to 100%, and that NOx is reduced. Not only can it be applied to a single burner or equipment installed with various types of burners (e.g. boilers, heating furnaces, indirators, incinerators, etc.), but it can also be applied to conventional burners in existing equipment, such as those mentioned above, by simply replacing the mixer. This is a highly practical method that can be easily modified.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明の方法に使用する燃料油供給筒の一例を
示す説明図であり、第2図(a)は従来法の又同図(1
))は本発明の方法の油滴燃焼機構をそれぞれ説明する
図である。 第1頁の続き @発明者 列目 雄之弼 新潟市松嗣35ooI地内 0発 明 者 堅 1) 秀 信 新潟市松浜町350
@地三菱瓦斯化学株式会社新潟工業所 三菱瓦斯化学株式会社新潟工業所
FIG. 1 is an explanatory diagram showing an example of a fuel oil supply cylinder used in the method of the present invention, and FIG.
)) are diagrams each illustrating the oil droplet combustion mechanism of the method of the present invention. Continuing from page 1 @ Inventor Column Yunosuke 35ooI Matsushi, Niigata City Inventor Ken 1) Hidenobu 350 Matsuhama-cho, Niigata City
@ Mitsubishi Gas Chemical Co., Ltd. Niigata Industrial Office Mitsubishi Gas Chemical Co., Ltd. Niigata Industrial Office

Claims (1)

【特許請求の範囲】[Claims] 混合器を内蔵する燃料油供給筒に、燃料油と噴霧媒体と
しての自燃性ガスを供給し、該自燃性ガスを上記燃料油
の助燃に用いることを特徴とする燃料油燃焼方法。
A fuel oil combustion method characterized in that fuel oil and a self-combustible gas as an atomizing medium are supplied to a fuel oil supply cylinder having a built-in mixer, and the self-combustible gas is used for auxiliary combustion of the fuel oil.
JP19612983A 1983-10-21 1983-10-21 Combustion method for fuel oil Pending JPS6089605A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19612983A JPS6089605A (en) 1983-10-21 1983-10-21 Combustion method for fuel oil

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19612983A JPS6089605A (en) 1983-10-21 1983-10-21 Combustion method for fuel oil

Publications (1)

Publication Number Publication Date
JPS6089605A true JPS6089605A (en) 1985-05-20

Family

ID=16352720

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19612983A Pending JPS6089605A (en) 1983-10-21 1983-10-21 Combustion method for fuel oil

Country Status (1)

Country Link
JP (1) JPS6089605A (en)

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